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NASA-LLIS-0162

Lessons Learned - Orbiter/ET Feedline Mating Stud Tensioner.

active, Most Current
Organization: NASA
Publication Date: 15 October 1992
Status: active
Page Count: 2
scope:

Description of Driving Event:

The orbiter/ET feedline mating stud tensioner unit exposes personnel to a high pressure source and could result in injury or flight hardware damage. During ratcheting of the nut onto the stud, personnel will be in the vicinity of high-pressure fluid, water, and rust inhibitor at 11,600 psig. Three stud tensioner heads, connected by six hoses through a common manifold, are used to apply a tension load of 64,000 lbs maximum to three cryogenic umbilical separation bolts by means of an air-driven hydraulic pumping unit.

Document History

NASA-LLIS-0162
October 15, 1992
Lessons Learned - Orbiter/ET Feedline Mating Stud Tensioner.
Description of Driving Event: The orbiter/ET feedline mating stud tensioner unit exposes personnel to a high pressure source and could result in injury or flight hardware damage. During ratcheting...
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